传感器故障检测、识别和适应方法

对现有的方法进行了研究，着重阐述用检测滤波器思想进行传感器故障检测、识别和适应的方法。并利用这些方法，对一个具体的模型设计一个传感器故障检测、诊断和适应系统。通过故障仿真计算，验证了本文提出的方法使用的有效性     

数控系统传感器故障检测隔离及适应技术

介绍一种发动机传感器故障的检测、隔离及适应方法，并给出某型涡轴发动机的数字仿真实例，说明该方法的有效性和实用性。     

用集成霍尔传感器设计智能计米器

工业中许多产品需要测量其长度 ,但传统的机械式计米器不能有效克服机械惯性 ,精度差 ,同时不能将长度信息进行管理 ,不适应当今信息化的生产环境。如采用集成霍尔传感器设计智能化计米器 ,能克服机械式的上述缺点。通过和上位计算机的通信可实现生产管理、销售。     

Attitude control system design and on-orbit performance analysis of nano-satellite––‘‘Tian Tuo 1’’

‘‘Tian Tuo 1'(TT-1) nano-satellite is the first single-board nano-satellite that was successfully launched in China. The main objective of TT-1 is technology demonstration and scientific measurements. The satellite carries out the significant exploration of single-board architecture feasibility validation, and it is tailored to the low-cost philosophy by adopting numerous commercialoff-the-shelf(COTS) components. The satellite is featured with three-axis stabilization control capability. A pitch bias momentum wheel and three magnetic coils are adopted as control actuators.The sun sensors, magnetometers and a three-axis gyro are employed as the measurement sensors.The quaternion estimator(QUEST) and unscented Kalman filter(UKF) method are adopted for the nano-satellite attitude determination. On-orbit data received by ground station is conducted to analysis the performance of attitude determination and control system(ADCS). The results show that the design of ADCS for TT-1 is suitable, robust and feasible.     

基于滑动时间窗主成分分析的液体火箭发动机传感器故障诊断方法

安装在发动机上的各种传感器是发动机状态监测的主要依据,由于工作环境恶劣,传感器失效时有发生。由于发动机运行过程中的性能蜕变和台次差异,现有基于主成分分析（PCA）的传感器故障隔离方法应用条件苛刻且诊断效果有限。针对这些问题,在对发动机数据分析的基础上,将滑动时间窗方法与PCA方法结合,提出双滑动时间窗的PCA方法用于故障传感器的隔离,并基于发动机试车数据进行了方法验证。结果表明：该方法能降低发动机性能蜕变和台次差异对发动机传感器故障诊断的影响,没有参数相关性的限制,可以实现对四种常见传感器故障的有效隔离,以及对两种发动机试验过程中故障的准确检测。研究证明了高速运转系统性能蜕变和强耦合复杂大系统台次差异对基于数据的故障诊断方法效果的影响,验证了在线学习/训练算法对这两种现象的鲁棒性。     

智能结构有限元模型的建立及静态形状控制

本文建立了含有分布压电传感元件和执行元件的板结构的有限元模型，提出了一种新的具有电自由度板弯曲单元，用于分析含有分布传感元件和执行元件的板结构。以此为基础，提出了智能结构静态形状控制的一般方法，即被动控制方法和主动控制方法。最后，提供了两个数值示例，说明本文提出的方法的应用。     

基于广播内存网络的无人机传感器仿真系统

讨论了一种基于广播内存网络的无人机飞行传感器仿真系统的设计与实现。系统硬件平台采用了基于网络的多机分布式体系结构。系统软件采用了VC＋＋6.0设计语言。该系统能够模拟无人机各种真实机载传感器信号及完成其它I／O信号处理，具有高实时性、高可靠性的特点。     

Didactic satellite based on Android platform for space operation demonstration and development

Space technology plays a pivotal role in society development. It offers new methods for telemetry, monitoring and control. However, this sector requires training, research and skills development but the lack of instruments, materials and budgets affects the ambiguity to understand satellite technology. The objective of this paper is to describe a demonstration prototype of a smart phone device for space operations study. Therefore, the first task was carried out to give a demonstration for spatial imagery and attitude determination missions through a wireless communication. The smart phone’s Bluetooth was used to achieve this goal inclusive of a new method to enable real time transmission. In addition, an algorithm around a quaternion based Kalman filter was included in order to detect the reliability of the prototype's orientation. The second task was carried out to provide a demonstration for the attitude control mission using the smart phone’s orientation sensor, including a new method for an autonomous guided mode. As a result, the acquisition platform showed real time measurement with good accuracy for orientation detection and image transmission. In addition, the prototype kept the balance during the demonstration based on the attitude control method.     

Non-destructive Evaluation of Composite Pressure Vessel by Using FBG Sensors

In recent years, advanced composite structures are used extensively in many industries such as aerospace, aircraft, automobile, pipeline and civil engineering. Reliability and safety are crucial requirements posed by them to the advanced composite structures be- cause of their harsh working conditions. Therefore, as a very important measure, structural health monitoring (SHM) in-service is defi- nitely demanded for ensuring their safe working in-situ. In this paper, fiber Bragg grating (FBG) sensors are surface-mounted on the hoop and in the axial directions of a FRP pressure vessel to monitor the strain status during its pressurization. The experimental results show that the FBG sensors could be used to monitor the strain development and determine the ultimate failure strain of the composite pressure vessel.     

航天器高精度姿态敏感器冗余测量信息智能融合技术

航天器在某些姿态敏感器故障的情况下，经多种组合进行自主故障判断、故障定位及重组后融合定姿，仍能保证姿测精度，或者在稍降低定姿精度的情况下，使航天器降级工作，挽救航天器。